Skyleader KP 2U User manual

SL200 FMM 2009-10-21
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SL200 FMM 2009-10-21
KP 2U
(
SK
YLEADER 200
)
Production number:
Registration mark:
Category: ULLa
Manufacturer: JIHLAVAN airplanes, s.r.o., Znojemská 826/64, 586 01 Jihlava, Czech Republic, European Union

SL200 FMM 2009-10-21
OWNER – OPERATOR OF THE AIRCRAFT:
Owner of the aircraft: The change of the ownership:
The change of the ownership:The change of the ownership:
Name:
Address:
Identity number:
Registration mark:
From, To:
Name:
Address:
Identity number:
Registration mark:
From, To:
Name:
Address:
Identity number:
Registration mark:
From, To:
Name:
Address:
Identity number:
Registration mark:
From, To:
KP 2U
(
SK
YLEADER 200
)

SL200 FMM 2009-10-21
5
CHAPTERS:
1. GENERAL INFORMATION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15
2. OPERATIONAL LIMITATIONS AND PERFORMANCE. . . . . . . . . . . . . . . . . . 35
3. STANDARD PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49
4. OTHER PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 67
5. EMERGENCY PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70
Book 1 FLIGHT MANUAL
Book 2 MAINTENANCE MANUAL
1. AIRCRAFT MAINTENANCE REGULATIONS . . . . . . . . . . . . . . . . . . . . . . . 81
2. WINGS AND HORIZONTAL TAIL UNIT DISMANTLING . . . . . . . . . . . . . . . . 91
3. LANDING GEAR DISMANTLING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 99
4. CHANGING FUEL FILTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .104
5. ELECTRIC WIRING DIAGRAM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .105
6. MAINTENANCE PLAN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .106

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CONTENTS:
1. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15
1.1. Prole of the company. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16
1.2. Equipment of the airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
1.3. Instrument panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19
1.4. Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
1.5. Amendments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
1.5.1. Amendments and supplements of the Flight Manual. . . . . . . . . . . . . 20
1.5.2. Amendments list . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
1.6. Abbreviations and denitions . . . . . . . . . . . . . . . . . . . . . . . . . . . 22
1.7. Basic technical data. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23
1.7.1. Technical description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23
1.7.2. Aircraft dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23
1.7.3. Deflections of the control surfaces. . . . . . . . . . . . . . . . . . . . . . . . . 24
1.7.4. Fuel tanks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24
1.7.5. Diagram of aircraft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25
1.8. Fluids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27
1.8.1. Rotax 912 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27
1.8.2. Rotax 914 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28
1.9. Propeller. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29
1.10. Instrument . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29
1.10.1. Operating switches of the left control stick . . . . . . . . . . . . . . . . . . . 29
1.10.2. Landing gear supervisory display . . . . . . . . . . . . . . . . . . . . . . . . . 30
Book 1 FLIGHT MANUAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

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1.10.3. Notices in the cockpit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30
2. OPERATIONAL LIMITATIONS AND PERFORMANCE . . . . . . . . . . . . . . . . 35
2.1. Structural regulations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35
2.2. General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35
2.3. Speeds . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 36
2.4. Take-o and landing distances . . . . . . . . . . . . . . . . . . . . . . . . . . 37
2.5. Climbing. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37
2.6. Gliding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38
2.7. Flight range. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38
2.8. Ceiling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 39
2.9. Manoeuvres approved. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 39
2.10. Engine limitations. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40
2.10.1. Rotax 912 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40
2.10.2. Rotax 914 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41
2.10.3. Other engines limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42
2.11. Fuel capacity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42
2.12. Wind and air operational limitations. . . . . . . . . . . . . . . . . . . . . . . 43
2.13. Weights and C-G limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44
2.13.1. Weight and Center of Gravity Limits charts . . . . . . . . . . . . . . . . . . . 45
2.14. Load factors. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47
2.15. Flight envelope . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47
2.16. Type of operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 48
2.17. Other limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 48
3. STANDARD PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49
3.1. Pre-ight inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49

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3.2. Aircraft maintenance after each ight . . . . . . . . . . . . . . . . . . . . . . 57
3.3. Procedures after cockpit entering . . . . . . . . . . . . . . . . . . . . . . . . 57
3.4. Starting the engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 58
3.5. Engine warm up and engine check . . . . . . . . . . . . . . . . . . . . . . . . 59
3.6. Procedures before taxiing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 59
3.7. Procedures on holding point . . . . . . . . . . . . . . . . . . . . . . . . . . . . 60
3.8. Start line procedures, take-o . . . . . . . . . . . . . . . . . . . . . . . . . . . 61
3.9. Downwind procedures. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61
3.10. Base leg procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 62
3.11. Procedures on nal approach, landing . . . . . . . . . . . . . . . . . . . . . 62
3.12. Procedures after landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 62
3.13. Engine shut down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 63
3.14. Leaving airplane. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 63
3.15. Check list of standard procedures . . . . . . . . . . . . . . . . . . . . . . . . 63
4. OTHER PROCEDURES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 67
4.1. Procedures for landing gear operation . . . . . . . . . . . . . . . . . . . . . 67
4.1.1. Signaling check before flight . . . . . . . . . . . . . . . . . . . . . . . . . . . . 67
4.1.2. Landing gear retraction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 68
4.1.3. Landing gear extension . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 68
4.2. Indicated conditions of wing aps and LG positions . . . . . . . . . . . . . 69
5. EMERGENCY PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70
5.1. Engine failure during rolling . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70
5.2. Engine failure after take-o . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70
5.3. Engine failure during ight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70
5.4. Emergency undercarriage extension. . . . . . . . . . . . . . . . . . . . . . . 72

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5.5. Emergency landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 72
5.6. Belly landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 73
5.7. Interrupted landing. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 73
5.8. Fire - on ground, engine not running. . . . . . . . . . . . . . . . . . . . . . . 73
5.9. Fire - on ground, engine running . . . . . . . . . . . . . . . . . . . . . . . . . 74
5.10. Fire - during ight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 74
5.11. Carburettor freezing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75
5.12. Engine and propeller vibrations. . . . . . . . . . . . . . . . . . . . . . . . . . 75
5.13. Emergency parachute system usage . . . . . . . . . . . . . . . . . . . . . . . 75
5.14. Check list of emergency procedures . . . . . . . . . . . . . . . . . . . . . . . 76
1. AIRCRAFT MAINTENANCE REGULATIONS . . . . . . . . . . . . . . . . . . . . . . 81
1.1. Periodic maintenance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 81
1.1.1. Inspection of control surfaces clearances . . . . . . . . . . . . . . . . . . . . 81
1.1.2. Maximal allowed control clearances. . . . . . . . . . . . . . . . . . . . . . . . 82
1.2. Lubrication of the aircraft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 82
1.3. Accumulator maintenance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 83
1.4. Hydraulic brakes settings and maintenance . . . . . . . . . . . . . . . . . . 84
1.4.1. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 84
1.4.2. Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 84
1.4.3. Refilling and deaerating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 84
1.4.4. Adjusting jaw clearances. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 85
1.4.5. Brake assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 86
1.5. Adjusting of control cables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 86
1.5.1. Changing cable adjusters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 87
Book 2 MAINTENANCE MANUAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 79

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1.6. The governor rectier circuit breaker . . . . . . . . . . . . . . . . . . . . . . 88
1.7. Locking hook adjusting and checking . . . . . . . . . . . . . . . . . . . . . . 89
2. WINGS AND HORIZONTAL TAIL UNIT DISMANTLING . . . . . . . . . . . . . . . 91
2.1. Removal of cover strip between wing and central section . . . . . . . . . 91
2.2. Removal and replacement of inspection covers. . . . . . . . . . . . . . . . 91
2.3. Removal of seats. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 92
2.4. Disassembly and assembly of outer wings . . . . . . . . . . . . . . . . . . . 92
2.4.1. Disassembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 92
2.4.2. Mark bolts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 93
2.4.3. Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 94
2.5. Disassembly and assembly of elevators. . . . . . . . . . . . . . . . . . . . . 96
2.6. Disassembly and assembly of stabilizer . . . . . . . . . . . . . . . . . . . . . 97
3. LANDING GEAR DISMANTLING . . . . . . . . . . . . . . . . . . . . . . . . . . . . 99
3.1. Removal of shock absorbers from main undercarriage . . . . . . . . . . . 99
3.2. Disassembly and assembly of main LG shock absorber . . . . . . . . . . . 99
3.3. Disassembly and assembly of main xed LG shock absorber . . . . . . 100
3.4. Front undercarriage shock absorber removal and assembly . . . . . . 101
3.5. Front undercarriage shock absorber disassembly and assembly . . . . 102
4. CHANGING FUEL FILTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .104
5. ELECTRIC WIRING DIAGRAM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .105
6. MAINTENANCE PLAN. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .106

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200
BOOK 1
FLIGHT MANUAL

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Flight Manual SL 200 Book 1
GENERAL INFORMATION1.
Dear Valued Customer!
Kindly accept our congratulations to the purchase of the UL/S-LSA aircraft SKYLEADER, which is a pure result of
our own research & development. Please remember - flying with SKYLEADER Aircraft is low-cost, safe and fun!
We believe that SKYLEADER Aircraft will satisfy your needs on more than 100%. As part of our continuing
commitment to responding to your needs, we continuously improve the quality of the products and services we
provide to all of our customers.
Team of SKYLEADER Aircraft is constantly looking for your satisfaction across a wide range of attributes such as
performance, product quality, service and repair, technical support, training, delivery and most importantly, your
overall satisfaction with SKYLEADER Aircraft.
Our company sincerely thank all of you who became our clients. Your continued feedback is invaluable to us, and
supports our endless quest in pursuing your Total Satisfaction.
Let us wish You and Your new SKYLEADER Aircraft all the best!
Sincerely,
Team of JIHLAVAN airplanes, s.r.o. („SKYLEADER Aircraft“)
www.skyleader.aero

Flight Manual SL 200 Book 1
SL200 FMM 2009-10-21
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Prole of the company1.1.
The company JIHLAVAN airplanes, s.r.o. was set up in March 2005after
complete takeover of all incorporeal rights and the complete
technology of production of the ultra-light aircraft from its predecessor
company Kappa 77 a.s..
Withthe usage of workers know-howthe companyJIHLAVANairplanes,
s.r.o., presented as SKYLEADER Aircraft, started the production of all-
metal UL/S-LSA aircraft under its own trade mark SKYLEADER 150,
SKYLEADER 200 and SKYLEADER 500.The primary goal of the company
was start the serial production and further research & development of
the aircraft.
SKYLEADER Aircraft regularly supplies the market and continues in organizational steps for the enlargement of the
production. With support of the Institute of Aerospace Engineering at the Brno University of Technology, CZ is the
aircraft developed and modernized all the time despite its existing top characteristics. The 3.200 m2 of modern
production area in the company Jihlavan, Inc. offers developing our activities in the future.
There are established trade contracts with the representatives in Italy, USA, South Africa, Taiwan, Germany, Poland, the
Netherlands, France, Spain, and many other countries. Its products are presented on the international exhibitions in
Friedrichshafen (Germany), Sun ´n Fun and Oshkosh (the USA), Rybnik (Poland), Blois (France), Cielo e Volo, Meeting
di Primavera (Italy) etc.
JIHLAVAN airplanes, s.r.o. developed the final production of WideBody model, which is now available on the market
under trademark SKYLEADER 200 and SKYLEADER 500. It takes the top flying qualities and extends the comfort of
crew by enlarging the cockpit on the maximum width along with the keeping of minimal operating costs and maximal
safety.

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Flight Manual SL 200 Book 1
Equipment of the airplane1.2.

Flight Manual SL 200 Book 1
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Flight Manual SL 200 Book 1
Instrument panel1.3.
See separate list: Instrument panel.

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Introduction1.4.
Validity: The Flight Manual is valid exclusively for the plane whose number is on the first page of the manual.
Amendments1.5.
Amendments and supplements of the Flight Manual1.5.1.
All amendments and supplements of the Flight Manual should be done as follows:
a) the manufacturer of UL aircraft sends an operational update with new and revised information to the owner of the
Flight Manual.
b) the holder of the Flight Manual is obliged:
1/ to change the original information with the revised edition, which is marked by the abbreviation„REV“
and the date of the change.
2/ to make a record of receiving the amendment into the amendment list. This list is found in art. B1-1.4.2..